I agree in the swept back wing. It takes postively effect at transsonic speeds, only. However, in the timeframe up to 1945, the germans developed more than this in the aerodynamic department:
deltawings
area rule
leading edge slots
wing boundary layers
bell shaped lift distibution for a stable flying wing
negative swept wing
variable wing geometry
basic understanding of faster than the speed of sound flight
This is making them the leaders in aerospace aerodynamics technology in my mind. The powerplant department can be divided by rocketry (germans, the US had an advantage with Goddart in an earlier timeframe) and jet engines (debatable).If you argue, that the Nene alone will make the British leading, than you miss my point. The Nene was kind of pinnacle of centrifugal flow design. Not a bad configuration, but limited. The BMW-018 axial engine was planned for the powerplant for bombers (Ju-287 to be more concrete), there was well probability to fit it under it´s wings. However it did not came to this. You know it. The F-9 is a POST WAR axial design, which benefitted from german experiances (esspecially the combustion chambers and turbine blade design). While it is true that it is based on the F-2, it was impossible with the british technology to field reliable axial jet engines with enough poweroutput during ww2. Unlike the germans. They did it. Think of the Jumo-004, imagine it would lead to more advanced engines based on it´s design in the 50´s. This is no argument, as is the argumant of the F-9. On the other side the DB-007 and Jumo-004 E are the most modern jet engines of ww2. Technologically more advanced than even the Nene or Dervent-V. They just had not the same poweroutput.
The british centrifugal flow engines are excellent in the timeframe till wars end, but these designs are not as advanced as axial designs. By the way, no british jet engine, centrifugal or not, was nearly produced in the numbers of the german axial engines during ww2. And the german design was far beyond british capabilities (afterburner, dual flow, fan)You can easily show a race if needed:
W-2B/early Dervents -BMW-003/Jumo-004B up to 2000 lbs of thrust
D.H. Ghost -DB-007 up to 3000 lbs of thrust
Dervent V -Jumo-004 E/H up to 4000 lbs of thrust
Nene -(Jumo-022) up to 6000 lbs of trhust
-BMW-018 up to 8000 lbs of thust
and because you need more, ()=never left it´s drawing board:
(DB-016) up to 28.600 lbs of thrust
And keep in mind that post war designs benefitted from excamination of german axial jet engine designs and construction charts of planned designs. It is interesting that british often refer the RB-39 of 1945 as the worlds first jet engine with diagonal (axial AND centrifugal) compressor (which actually was the german HeS-011) and dual flow (which was indeed
the german DB-007). You can argue that the german designs are not reliable or that they faced big problems to hit even 3000 lbs, not to speak of 5000 lbs. All agreed, but they are under no circumstances BEHIND the british jet engine development during ww2. Indeed they have been more innovative in many ways.
Sources to Rolls Royce Nene:
www.tanks45.tripod.com/Jets45/List of engine:
quote:
"...the "R.B. 41 Nene", which was first bench tested in november 1944 well making over 4000 lbs of thrust..."
Compare also the soviet development of Nene copies: RD 45 (based on UK sold Nene) and VK-1 (improved by means of better heat resistent materials) show a significant thrust difference. The development of Nene 1-10 surely not decreased fuel consumption, only.
I will source the net for further sources, if needed. Additional articles supporting that the Nene in 1944 did not made (but was capable to) 5000 lbs of thrust:
G. Norman, A comprehensive analysis of soviet post war jet engines up to the mid 50´s, in: L.H. Behrens, Probleme zur frühen Strahltriebwerkentwicklung, AVA (Stuttgart 1972), page 312-387.
P. le Goyet, Évolution de l´aviation entre 1939 et 1945, in: Revue d´histoire de la deuxieme guerre mondiale, Vol. 73 (Paris 1969), passim.
D. Richards/H.S.George Saunders, Royal Air Force 1939-1945, Vol. III (London 1953), page 56f.